Recent Experiments on Hypersonic Combustion in an Expansion Tube Test Facility

Author:

Erdos John I.

Publisher

Springer Netherlands

Reference22 articles.

1. Anderson, G., Kumar, A., and Erdos, J., 1990. “Progress in hypersonic combustion technology with computation and experiment,” AIAA 90–52,54.

2. Anderson, R. C., Trucco, R. E., Rubin, L. F., and Swain, D. M., 1992. “Visualization of hydrogen injection in a scramjet by simultaneous PLIF and laser holographic imaging,” Proc. 1992 NASA Langley Measurement Technology Conference, NASA CP 3161.

3. Bakos, R., Morgan, R., and Tamagno, J., 1992. “Effects of oxygen dissociation on hypervelocity combustion experiments,” AIAA 92–3964.

4. Bakos, R., Tamagno, J., Rizkalla, O., Pulsonetti, M., Chinitz, W., and Erdos, J., 1992. “Hypersonic mixing and combustion studies in the hypulse facility,” J. Prop. Power 8(4), pp. 900–906.

5. Bakos, R., Tamagno, J., Trucco, R., Rizkalla, O., Chinitz, W., and Erdos, J., 1992. “Mixing and combustion studies using discrete orifice injection at hypervelocity flight speeds,” J. Prop. Power 8(6), pp. 1260–1296.

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1. Characterization of Expansion Tube Flows for Hypervelocity Combustion Studies;Journal of Propulsion and Power;2002-07

2. Hypervelocity combustion studies using simultaneous OH-PLIF and Schlieren imaging in an expansion tube;35th Joint Propulsion Conference and Exhibit;1999-06-20

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4. Cavity flameholders for ignition and flame stabilization in scramjets - Review and experimental study;34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;1998-07-13

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